Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

European Retrievable Carrier

From Wikipedia, the free encyclopedia
ESA space science satellite
European Retrievable Carrier
EURECA deployment in 1992
Mission typeMaterials science
Astronomy
OperatorESA
COSPAR ID1992-049BEdit this at Wikidata
SATCATno.22065
Mission durationPlanned: 1 year
Elapsed: 334 days
Spacecraft properties
ManufacturerMBB-ERNO
Launch mass4,491 kilograms (9,901 lb)
Power1,000 watts
Start of mission
Launch date31 July 1992, 11:56:48 UTC
RocketSpace Shuttle Atlantis
STS-46
Launch siteKennedyLC-39B
Deployment date2 August 1992 (1992-08-02)
End of mission
DisposalRecovered
Recovered bySpace Shuttle Endeavour
STS-57
Recovery date1 July 1993 (1993-08)
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Eccentricity0.00066
Perigee altitude438 kilometres (272 mi)
Apogee altitude447 kilometres (278 mi)
Inclination28.5 degrees
Period93.4 minutes
Epoch2 August 1992, 20:00:00 UTC[1]

TheEuropean Retrievable Carrier (EURECA) was an uncrewed 4.5-tonne satellite with 15 experiments.[2] It was aEuropean Space Agency (ESA) mission and the acronym was derived fromArchimedes' bathtub revelation "Eureka!".

It was built by the GermanMBB-ERNO and had automatic material science cells as well as small telescopes for solar observation (including x-ray).

It was launched 31 July 1992 bySpace Shuttle Atlantis duringSTS-46, and placed into an orbit at an altitude of 508 km (316 mi). EURECA was retrieved on 1 July 1993 bySpace Shuttle Endeavour duringSTS-57 and returned to Earth. It was designed to fly five times with different experiments but the following flights were cancelled.

EURECA is one of the few uncrewed space vehicles that have been returned to the Earth unharmed. It has been on display at theSwiss Museum of Transport inLucerne since 2000.[3]

Design

[edit]
EURECA retrieval in 1993

EURECA was made of high-strength carbon-fiber struts andtitanium nodal points joined together to form a framework of cubic elements. Thermal control on EURECA combined both active and passive heat transfer and radiation systems. Active heat transfer was achieved by means of afreon cooling loop which dissipated the thermal load through two radiators into space. The passive system made use of multilayer insulation blankets combined with electrical heaters.

The electrical subsystem was powered by deployable and retractable solar arrays together with four 40 amp-hournickel-cadmium batteries. When EURECA was in the Shuttle cargo bay, power was supplied by the Shuttle. The modular attitude and orbit control subsystem (AOCS) maintained attitude and spacecraft orientation and stabilization. An orbit transfer assembly, consisting of four thrusters, was used to boost EURECA to its operational attitude of 515 km (320 mi) and return it to a retrievable orbit of about 300 km (190 mi).

EURECA was three-axis stabilized by means of a magnetic torque assembly together with a nitrogen reaction control assembly (RCA). Data handling was carried out by EURECAs data handling subsystem (DHS) supported by telemetry and command subsystems providing the link to the ground station.

Experiments

[edit]

EURECA consisted of 15 experiments:[4][5]

  • Solution Growth Facility (SGF) (Belgium, Denmark, Norway)BelgiumDenmarkNorway
  • Protein Crystallization Facility (PCF) (Germany)Germany
  • Exobiology Radiation Assembly (ERA) (Germany)Germany
  • Multi-Furnace Assembly (MFA) (Italy)Italy
  • Automatic Mirror Furnace (AMF) (Germany)Germany
  • Surface Forces Adhesion Instrument (SFA) (Italy)Italy
  • High Precision Thermostat Instrument (HPT) (Germany)Germany
  • Solar Constant and Variability Instrument (SOVA) (Belgium)Belgium
  • Solar Spectrum Instrument (SOSP) (France)France
  • Occultation Radiometer Instrument (ORI) (Belgium)Belgium
  • Wide Angle Telescope for Cosmic Hard X-rays (WATCH) (Denmark)Denmark
  • Timeband Capture Cell Experiment (TICCE) (Great Britain)United Kingdom
  • Radio Frequency Ionization Thruster Assembly (RITA) (Germany)Germany
  • Inter-Orbit Communications (IOC) (France/the Netherlands)FranceNetherlands
  • Advanced Solar Gallium Arsenide Array (ASGA) (Italy)Italy

The WATCH instrument observed Cosmic X-rays in an extremely wide field of view, a 65 degree range capable of observing 1/4 of the sky.[6] The design is a Rotation Modulation Collimator, in which stripes of NaI(Tl) and CsI(Na) detectors make aphoswich.[7]

Results

[edit]

WATCH monitored about 25 X-rays sources over the whole sky over the course of the mission, as well as detecting 19 cosmic gamma ray bursts.[8] Many of the gamma ray bursts were able to be localized to within 1 degree.[9]

In the summer of 2016, EURECA was transported to theSwiss Federal Laboratories for Materials Science and Technology (Empa) in Dübendorf near Zurich where X-ray scans of the satellite were taken. The goal was to find out how EURECA's 11-month exposure to space had affected its structure and selected experiments it carried.[10] EURECA was then brought back to the Swiss Museum of Transport in Lucerne and has since been exhibited in a new way, with both solar panels fully deployed for the first time.[11]

See also

[edit]

References

[edit]
  1. ^"NASA – NSSDCA – Spacecraft – Trajectory Details".nssdc.gsfc.nasa.gov.Archived from the original on 2019-07-26. Retrieved2018-05-01.
  2. ^"Eureca"(PDF). Archived fromthe original(PDF) on 2007-09-30. Retrieved2011-04-12.
  3. ^"From Space to Lucerne".Eureca – a satellite on the road (again)!.Archived from the original on 19 May 2020. Retrieved5 June 2017 – via YouTube.
  4. ^EURECA Scientific Results, Advances in Space Research, Vol. 16, Issue 8 (1995) 1–140.
  5. ^"The European Retrievable Carrier (EURECA) mission".Archived from the original on 2020-10-18. Retrieved2020-11-09.
  6. ^"The European Retrievable Carrier (EURECA) mission".heasarc.gsfc.nasa.gov.Archived from the original on 2019-07-26. Retrieved2018-07-23.
  7. ^"The European Retrievable Carrier (EURECA) mission".heasarc.gsfc.nasa.gov.Archived from the original on 2019-07-26. Retrieved2018-07-23.
  8. ^"The European Retrievable Carrier (EURECA) mission".heasarc.gsfc.nasa.gov.Archived from the original on 2019-07-26. Retrieved2018-07-23.
  9. ^"The European Retrievable Carrier (EURECA) mission".heasarc.gsfc.nasa.gov.Archived from the original on 2019-07-26. Retrieved2018-07-23.
  10. ^"Eureca X-Ray Scan".Eureca – a satellite on the road (again)!.Archived from the original on 22 April 2020. Retrieved5 June 2017 – via YouTube.
  11. ^"EURECA's last journey to Empa and back to Lucerne".Eureca – a satellite on the road (again)!.Archived from the original on 23 April 2020. Retrieved5 June 2017 – via YouTube.

External links

[edit]
Wikimedia Commons has media related toEURECA.
General
Facilities
Earth-based
activities
Companies
Crewed
spacecraft
Active
Planned &
proposed
Retired
Cancelled
Space
stations
Active
Planned &
proposed
Retired
Cancelled
Cargo
spacecraft
Planned &
proposed
Retired
Missions
Space
Shuttle
Mir
ISS
(commercial)
Space Centres
Launch vehicles
Facilities
Communications
Programmes
Predecessors
Related topics
Science
Astronomy
& cosmology
Earth
observation
Planetary
science
Solar
physics
Human
spaceflight
Telecommunications
and navigation
Technology
demonstration
and education
Launch
and reentry
Proposed
Cancelled
Failed
Future missions initalics
January
February
March
April
May
June
July
August
September
October
November
December
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
Current
Past
Planned
Proposed
Cancelled
Lost
Sun-Earth
International
National
Retrieved from "https://en.wikipedia.org/w/index.php?title=European_Retrievable_Carrier&oldid=1299560255"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp